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  4. Variations on R-curves and traction-separation relations in DCB specimens loaded under end opening forces or pure moments
 
research article

Variations on R-curves and traction-separation relations in DCB specimens loaded under end opening forces or pure moments

Pappas, Georgios A.  
•
Botsis, John  
May 15, 2020
International Journal Of Solids And Structures

In this work the differences in R-curve response and traction-separation relations due to a finite damage zone or large-scale bridging (LSB) in mode I fracture on double cantilever beams (DCB) were investigated under end opening forces (EOF) and pure moments (PM). To realize PM loading, a novel test-rig was designed, built and used to test adhesive joints with metallic substrates and unidirectional carbon fiber reinforced polymer (CFRP) specimens. In the adhesive joints, no pronounced difference was observed between the R-curves due to the two loading conditions. However, the experiments on the CFRP specimens showed important differences on both R-curve and traction separation relations due to LSB when comparing EOF and PM loading. These differences are attributed to the different curvature of the specimens' arms in EOF and PM allowing for longer bridging zone in the latter case. The increase in the energy release rates was similar to 40% for the specimens subjected to PM with about four times higher maximum crack opening displacements at the steady state. Pertinent cohesive zone simulations predict the respone very well. (C) 2019 Elsevier Ltd. All rights reserved.

  • Details
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Type
research article
DOI
10.1016/j.ijsolstr.2019.11.022
Web of Science ID

WOS:000526811800004

Author(s)
Pappas, Georgios A.  
Botsis, John  
Date Issued

2020-05-15

Publisher

PERGAMON-ELSEVIER SCIENCE LTD

Published in
International Journal Of Solids And Structures
Volume

191

Start page

42

End page

55

Subjects

Mechanics

•

Mechanics

•

laminated composites

•

adhesive joints

•

traction separation relations

•

pure moment

•

end opening forces

•

cohesive zone modeling

•

delamination resistance

•

crack-growth

•

composites

•

fracture

•

interlaminar

Editorial or Peer reviewed

REVIEWED

Written at

EPFL

EPFL units
LMAF  
Available on Infoscience
May 2, 2020
Use this identifier to reference this record
https://infoscience.epfl.ch/handle/20.500.14299/168519
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